STARLINK-31640 (59748)

COSPAR: 2024-090U | Alt Name: Starlink 31640

Image
STARLINK-31640 Satellite Image
Additional Sources
Launch Details

Launch Date

May 13, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59748

International Designator

2024-090U

Epoch

Sun, 19 Jul 2026 20:41:37 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

157.10°

Eccentricity

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Argument of Perigee

270.50°

Period

94.27 min

Mean Motion

15.28 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot
3D Visualization
Basic Satellite Info

Name

STARLINK-31640

Alternative Name

Starlink 31640

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59748U 24090U   26200.86224382  .00000805  00000+0  38771-4 0  9995
2 59748  43.0030 157.1020 0000859 270.4976  89.5777 15.27566383123654

Source: Celestrak

Summary
The STARLINK-31640 satellite, also known as Starlink 31640, is a communication satellite under the Starlink v2 Mini configuration and part of the Starlink Group 6-58-19 mission. Launched on May 13, 2024, from the AFE launch site (LC40) using a Falcon 9 rocket, it has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. The satellite's dry mass is 700 kilograms and its launch mass was 730 kilograms. Equipped with Argon ion thrusters for propulsion, Ku/Ka/E-band payload, and an optical inter-satellite link, it relies on solar arrays and batteries for power. Manufactured by SPXS, the satellite's purpose is communication and is owned by the same entity.

Starlink is a satellite constellation developed by SpaceX with the aim of providing global broadband internet coverage. Thousands of small satellites are deployed in low Earth orbit (LEO), enabling high-speed internet access even in remote areas. However, the rapid increase in satellites raises concerns about space debris and the potential for collisions, which can lead to further debris creation and endanger other spacecraft. Additionally, the sheer number of Starlink satellites can affect astronomical observations by increasing light pollution. Proper deorbiting plans and international coordination are essential to mitigate these challenges and ensure long-term sustainability in space.
Physical Characteristics

Length

0.3

Diameter

4.1

Span

29

Dry Mass

700

Launch Mass

730

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 6-58-19

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Starlink v2 Mini

Motor

Argon ion thrusters

Equipment

Ku/Ka/E-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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